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VELOX P1, P2

VELOX-P2 [TU München]

VELOX-P is a 1U CubeSat mission by Nanyang Technological University, Singapore, to develop and orbit a CubeSat for technology demonstration, to test in-house attitude determination and control system, power subsystem, and to support a dual-FOV sun sensor payload. The Cubesat VELOX Pwill be launched into experimental high inclination circular orbit at 300 km on an Interorbital Neptune flight from off-shore California with a number of other spacecraft. For its 8-12 weeks in orbit, VELOX P will log telemetry data from its various subsystems and send them down to our mission control center for analysis. As the Neptune launch vehicle is much delayed, a launch date can not be estimated.

VELOX-P2 is also 1U cubesat mission for technology demonstration to test in house ADAC system, power sub-system and to support a dual FOV suns sensor payload.

Nation: Singapore
Type / Application: Technology
Operator: Nanyang Technological University, Singapore
Contractors: Nanyang Technological University, Singapore
Equipment:
Configuration: CubeSat (1U)
Propulsion: None
Power: Solar cells, batteries
Lifetime:
Mass: 1 kg
Orbit: 593 km × 699 km, 97.80° (#2)
Satellite COSPAR Date LS Launch Vehicle Remarks
VELOX-P - ? ? Neptune with ?
VELOX P2 2013-066Y 21.11.2013 Do LC-370/13 Dnepr with DubaiSat 2, STSAT 3, WNISAT 1, SkySat 1, BRITE-PL, AprizeSat 7, AprizeSat 8, UniSat 5, Delfi-n3Xt, Dove 3, Dove 4, Triton 1, CINEMA 2, CINEMA 3, CubeBug 2, GOMX 1, NEE 02 Krysaor, FUNcube 1, HiNCube, ZACUBE 1, ICube 1, HumSat-D, PUCP-SAT 1, First-MOVE, UWE 3, Pocket-PUCP, BeakerSat 1, QubeScout S1, $50SAT, Wren, BPA 3

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